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GB1514096A - Axial flow rotor or stator assembly - Google Patents

Axial flow rotor or stator assembly

Info

Publication number
GB1514096A
GB1514096A GB453176A GB453176A GB1514096A GB 1514096 A GB1514096 A GB 1514096A GB 453176 A GB453176 A GB 453176A GB 453176 A GB453176 A GB 453176A GB 1514096 A GB1514096 A GB 1514096A
Authority
GB
United Kingdom
Prior art keywords
blades
fan
auxiliary
main
rotor
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired
Application number
GB453176A
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Rolls Royce PLC
Original Assignee
Rolls Royce PLC
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Rolls Royce PLC filed Critical Rolls Royce PLC
Priority to GB453176A priority Critical patent/GB1514096A/en
Publication of GB1514096A publication Critical patent/GB1514096A/en
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D19/00—Axial-flow pumps
    • F04D19/02—Multi-stage pumps
    • F04D19/028—Layout of fluid flow through the stages
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12—Blades
    • F01D5/14—Form or construction
    • F01D5/141—Shape, i.e. outer, aerodynamic form
    • F01D5/142—Shape, i.e. outer, aerodynamic form of the blades of successive rotor or stator blade-rows
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12—Blades
    • F01D5/14—Form or construction
    • F01D5/141—Shape, i.e. outer, aerodynamic form
    • F01D5/146—Shape, i.e. outer, aerodynamic form of blades with tandem configuration, split blades or slotted blades
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
    • F02K3/02—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber
    • F02K3/04—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
    • F02K3/02—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber
    • F02K3/04—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type
    • F02K3/06—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type with front fan

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

1514096 Gas turbine ducted fan engines ROLLS-ROYCE Ltd 1 Feb 1977 [5 Feb 1976] 04531/76 Headings F1C and F1J In a gas turbine ducted fan engine comprising a row of fan rotor blades 14, a row of auxiliary rotor blades 16 is mounted on the fan rotor 12, the auxiliary fan blades being enshrouded and being of less radial extent than the main fan blades 14, each auxiliary blade being disposed so as to lie downstream of the space between two main fan blades 14. The object of the invention is to provide some compression of the air passing to the engine compressor 11, the inner postion of the main fan blades providing little or no compression. Auxiliary stator blades may similarly be provided downstream of main stator blades.
GB453176A 1977-02-01 1977-02-01 Axial flow rotor or stator assembly Expired GB1514096A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB453176A GB1514096A (en) 1977-02-01 1977-02-01 Axial flow rotor or stator assembly

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB453176A GB1514096A (en) 1977-02-01 1977-02-01 Axial flow rotor or stator assembly

Publications (1)

Publication Number Publication Date
GB1514096A true GB1514096A (en) 1978-06-14

Family

ID=9778953

Family Applications (1)

Application Number Title Priority Date Filing Date
GB453176A Expired GB1514096A (en) 1977-02-01 1977-02-01 Axial flow rotor or stator assembly

Country Status (1)

Country Link
GB (1) GB1514096A (en)

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2000003136A1 (en) * 1998-07-09 2000-01-20 Pratt & Whitney Canada Corp. Integrated fan/low pressure compressor rotor for gas turbine engine
US20160186772A1 (en) * 2014-12-29 2016-06-30 General Electric Company Axial compressor rotor incorporating non-axisymmetric hub flowpath and splittered blades
US20180017019A1 (en) * 2016-07-15 2018-01-18 General Electric Company Turbofan engine wth a splittered rotor fan
US9874221B2 (en) 2014-12-29 2018-01-23 General Electric Company Axial compressor rotor incorporating splitter blades
EP3828384A1 (en) * 2019-11-26 2021-06-02 Rolls-Royce plc Gas turbine engine
US11149552B2 (en) 2019-12-13 2021-10-19 General Electric Company Shroud for splitter and rotor airfoils of a fan for a gas turbine engine
US12037921B2 (en) 2022-08-04 2024-07-16 General Electric Company Fan for a turbine engine

Cited By (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2000003136A1 (en) * 1998-07-09 2000-01-20 Pratt & Whitney Canada Corp. Integrated fan/low pressure compressor rotor for gas turbine engine
US6145300A (en) * 1998-07-09 2000-11-14 Pratt & Whitney Canada Corp. Integrated fan / low pressure compressor rotor for gas turbine engine
US20160186772A1 (en) * 2014-12-29 2016-06-30 General Electric Company Axial compressor rotor incorporating non-axisymmetric hub flowpath and splittered blades
US9874221B2 (en) 2014-12-29 2018-01-23 General Electric Company Axial compressor rotor incorporating splitter blades
US9938984B2 (en) * 2014-12-29 2018-04-10 General Electric Company Axial compressor rotor incorporating non-axisymmetric hub flowpath and splittered blades
US20180017019A1 (en) * 2016-07-15 2018-01-18 General Electric Company Turbofan engine wth a splittered rotor fan
WO2018084902A1 (en) * 2016-07-15 2018-05-11 General Electric Company Turbofan engine and corresponding method of operating
EP3828384A1 (en) * 2019-11-26 2021-06-02 Rolls-Royce plc Gas turbine engine
CN112943689A (en) * 2019-11-26 2021-06-11 劳斯莱斯有限公司 Gas turbine engine
US11339727B2 (en) 2019-11-26 2022-05-24 Rolls-Royce Plc Gas turbine engine
US11149552B2 (en) 2019-12-13 2021-10-19 General Electric Company Shroud for splitter and rotor airfoils of a fan for a gas turbine engine
US12037921B2 (en) 2022-08-04 2024-07-16 General Electric Company Fan for a turbine engine

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Legal Events

Date Code Title Description
PS Patent sealed
PCNP Patent ceased through non-payment of renewal fee